Direct Dial: 703.760,5204 

kpomfret a williamsmullen.com 

September 11, 2015 

ELCCTRONIC SIJBMISSION 

U.S. Department of Transportation, Docket Operations 

West Building, Ground Floor, Room W12-140 

1200 New Jersey Ave., SE 

Washington, D.C. 20590 

Re: Section 333 Exemption Request 

Dear Sir or Madam: 

Pursuant to Section 333 of the FAA Modernization and Reform Act of 2012 (the 

"Reform Act"), Pictometry International Corp. ("Petitioner") hereby applies for an exemption 

from the Federal Aviation Regulations ("FARs") described in Section VII below, a Certificate of 

Waiver and Authorization ("COA") and any other exemptions necessary to allow the Petitioner 

to operate the small Unmanned Aircraft Systems ("UAS") described in Section IV for 

commercial aerial data collection purposes, as more fully described in Section III below. 

I.Background on Petitioner 

Pictometry International Corp., an EagleView company, invented the technology behind 

georeferenced aerial oblique image capture, providing powerful high-resolution aerial imagery 

and analytical tools for assessment, GIS, public safety, emergency response and overall 

visualization needs. It has been the market leader for over 12 years in the government space, with 

a fleet of 89 aircraft, and with over 1,100 county customers, as well as state and, federal 

(including Department of Homeland Security and Civil Air Patrol), and local customers. The 

company also services infrastructure, insurance and other commercial industries. The company 

is a leader in providing aerial imagery to the public safety community with its 9-1-1 integrations, 

post disaster aerial imaging and search and rescue tools. 

2891431 1 . ,_1 

8300 Greensboro Drive, Suite 1100 Tysons Corner, VA 22102 T 703.760.5200 F 703.748.0244 

williamsmullen.com I A Professional Corporation 
U.S. Department of Transportation, Docket Operations 

September 11, 2015 

Page 2 

II.Contact Information 

The contact information for Petitioner is set forth below: 

Charles Mondello 

President, Property Drone Consortium, Co. and 

Chief Strategist, EagleView Technology Corp. 

100 Town Center Drive 

Rochester NY 14623 

III. Pronosed Uses of UAS 

Petitioner is requesting the exemption to use the UAS for several commercial 

purposes. These include: 

A. Commereial and Residential Building Inspection 

Petitioner proposes to use the UAS to inspect commercial and residential buildings and 

property under controlled conditions. These conditions will include (i) obtaining the permission 

of the owners of the property or authorized representatives, (ii) utilizing geofencing when 

available, and (iii) taking steps to protect persons and propei -ty. The purpose of these operations 

will be to gather various types of data on the buildings and property to incorporate into 

Petitioner's workflow and products. 

B. Infrastructure Inspection 

Petitioner also proposes to use the UAS to monitor and inspect tixed assets, infrastructure 

and equipment for the energy, telecommunications and transportation industries such as 

pipelines, towers and lines of communication and transportation. These operations will also be 

conducted under controlled conditions, which will include obtaining the permission of property 

owners or authorized representatives, geofencing and safety measures for persons and property. 

C. Pre/post-Disaster Data Collection 

Petitioner also wishes to utilize the UAS to collect data both prior to and following 

natural disasters such as hurricanes, fires and floods. Petitioner recognizes the need to balance 

the value of that data to first responders and other parties, with the need to defer to those 

conducting search and rescue operations. As a result, Petitioner will coo.rdinate with appropriate 

government authorities (federal, state and local) as well as appropriate aviation authorities and 

will defer to those authorities at all times. 

28914311__1 
WILLIAMS MULLEi--4 

U.S. Department of Transportation, Docket Operations 

September 11, 2015 

Page 3 

In addition, Petitioner proposes to use the UAS for other types of aerial data collection as 

permitted by the Administrator under Section 333. Such aerial data collection shall include any 

remote sensing and measuring by an instrument(s) aboard the UAS. 

Since there are no novel issues associated with the use of the UAS for these purposes, the 

Petitioner requests that this request for exemption be considered on an expedited basis. In that 

regard, Petitioner notes that the FAA has previously granted exemptions for the UAS. 

IV. Unmanned Aircraft Systems 

This petition is to operate the UAS listed on Attachment 1 attached hereto, all of which 

weigh less than 55 pounds including payload and have been previously approved by the 

Administrator for operation under Section 333. 1 

V. Statutory Authority for Reguested Exemptions 

This petition for exemption is submitted in accordance with Section 333 of the Reform 

Act. Pursuant to Section 333 of the Reform Act, the Federal Aviation Administration (FAA) 

Administrator (the "Administrator") is to permit operation of an unmanned aireraft system where 

it does not create a hazard to users of the national airspace system (NAS) or the public or pose a 

threat to national security. Moreover, the Federal Aviation Act grants the Administrator general 

authority to grant exemptions from the agency's safety regulations and minimum standards when 

the Administrator decides such a requested exemption is in the public interest. See 49 U.S.C. 

§§ 106(f), 44701-44716, et seq. A party requesting an exemption must explain the reasons why 

the exemption: (i) would benefit the public as a whole, and (ii) would not adversely affect safety 

or how it would provide a level of safety at least equal to the existing rules. 14 C.F.R. § 11.81. 

VI. Safety Measures and Public Interest Benefits 

As described in more detail in Section IX, the Petitioner will take measures to ensure 

such operations will not create a hazard to aviation or the public. Flights will be conducted 

under 400 feet AGL thereby avoiding interference with users of the NAS. Flights will be 

suspended immediately to yield right-of-way to any other aircraft. Geo-fencing will be utilized 

when available to ensure that a UAS does not fly outside of the intended area. Given the size 

and speed of the tJAS, the controlled nature of the locations being used and the lack of explosive 

materials or flammable jet fuels, the operations will not pose a threat to national security. 

There are a number of reason.s why granting the Petitioner's request to operate the UAS 

for these commercial aerial data collection purposes is in the public interest. For example, use of 

UAS for inspecting commercial and residential buildings and property will make conditions for 

1 Petitioner notes that this is the same list of UAS included in the grant issued by the Administrator in Exemption No 

12646 on August 28, 2015. 

zs91as11 1 
U.S. Department of Transportation, Docket Operations 

September 11, 2015 

Page 4 

insurance claim representatives safer. Today claim representatives must climb onto a roof for 

data collection. Such activities are inherently dangerous as each year claim handlers are injured 

due to falls from roofs. Claim handlers will be able to reduce their exposure to such hazards by 

using a UAS. In addition, they will be able to obtain the data necessary to make accurate 

assessments of a roof more quickly. Similarly, utilization of UAS to inspect construction, 

telecommunication and energy physical assets will result in enhanced safety for individuals, cost 

savings and greater efficiencies in large and critical industries. Use of the UAS during natural 

disasters will ensure first responders receive critical information in a timely manner. It will also 

allow insurance companies to process claims more quickly without requiring their personnel to 

work in an environment strewn with debris and other hazards. 

VII. Specific Sections from Which Petitioners Seek an Exemption 

Based upon the information provided and the exemptions that the FAA has already 

granted pursuant to Section 333, the Petitioner requests the following exemptions: 

14 C.F.R. § 61.23(a) 

14 C.F.R. § 61.23(c) 

14 C.F.R. § 61.101(e)(4) 

14 C.F.R. § 61.101(e)(5) 

14 C.F.R. § 61.113(a) 

14 C.F.R. § 61.315(a) 

14 C.F.R. § 91.7(a) 

14 C.F.R. § 91.119(c) 

14 C.F.R. § 91.121 

14 C.F.R. § 91.1.51(a)(1) 

14 C.F.R. § 91.405(a) 

14 C.F.R. § 91.407(a)(1) 

14 C.F.R. § 91.409(a)(1) 

14 C.F.R. § 91.409(a)(2) 

14 C.F.R. § 91.417(a) 

14 C.F.R. § 91.417(b) 

VIII. Justifications for Each Exemption Reguest 

l.14 C F R§ 61 23(a) 14 C F R§ 61 23(c) 14 C F R§ 61 101(e)(4) 14 C.F.R. 

§ 1.101(e)(5) 14 C.F.R. §61.113(a) and 14 C.F.R. § 61.315(a). 6

Petitioner notes that FAA is now requiring the PIC to hold either an airline transport, 

commercial, private, recreational or sport certificate pilot license and either a current FAA 

airman medical certificate or a valid U.S. driver's license issued by a state, the District of 

Columbia, Puerto Rico, a territory, a possession, or the Federal government. Petitioner will 

ensure that its PICs will satisfy each of these requirements. Since Petitioners' PICs will be 

289143 „1 
LVAM111 AEff 

U.S. Department of Transportation, Docket Operations 

September 11, 2015 

Page 5 

operating UAS under the same conditions as those previously granted, an equivalent level of 

safety will be met by granting these exemptions. 

2. 14 C.F.R. 91.7(a) Civil aircraft worthiness . 

Section 91.7(a) requires that an operator determine an aircraft is in airworthy condition 

before a flight. Petitioner requests relief from this section provided that the operator of the UAS 

determines prior to each flight that the aircraft is in compliance with the operational documents 

of the applicable UAS (the "Operational Documents"). Such pre-flight inspection will provide 

the equivalent level of safety as that provided by this section. Petitioner notes that the 

Administrator has granted relief from this section in previous exemptions. 

3. 14 C.F.R. 91.119(c) Minimum safe altitudes over congested and other areas . 

Section 91.119(c) establishes safe altitudes for operation of civil aircraft over areas other 

than congested areas. The Petitioner requests relief from this section with respect to those 

participating persons, vehicles, and structures directly involved operations. The UAS will never 

operate at higher than 400 AGL. Relief from this section is warranted as operations will be 

conducted with adequate safety provisions as outlined herein and in the applicable Operational 

Documents. As a result, an equivalent level of safety will be met by granting this exemption. 

Petitioner notes that the Administrator has granted relief from this section in previous 

exemptions. 

4. 14 C.F.R. ~ 91.121 Altimeter Settings. 

This regulation requires each person operating an aircraft to maintain cruising altitude by 

reference to an altimeter that is set ". .. to the elevation of the departure airport or an appropriate 

altimeter setting available before departure." An exemption from section may be needed if the 

UAS does not have a barometric altimeter but instead has a GPS altitude read out. An equivalent 

level of safety will be achieved by the operator, pursuant to the applicable Operational 

Documents, confirming the altitude of the launch site shown on the GPS altitude indicator before 

flight. As a result, an equivalent level of safety will be met by granting this exemption. 

Petitioner notes that the Administrator has granted relief from this section in previous 

exemptions. 

14 C.F.R. § 91.151(a)(1) Fuel requirements for flight in VFR conditions . 

Section 91.151 (a)(1) prohibits an individual from beginning "a flight in an airplane 

under VFR conditions unless (considering wind and forecast weather conditions) there is enough 

fuel to fly to the first point of intended landing, and, assuming normal cruising speed —(1) 

During the day, to fly after that for at least 30 minutes." 

Complying with the 30 minute reserve would severely limit the length of the Petitioner's 

UAS flights and hamper operational use. Given the limitations on the UAS's proposed flight 

289143111 
1~~/~\u~-~ul~l~~~1~ 

U.S. Department of Transportation, Docket Operations 

September 11, 2015 

Page 6 

area, a longer time frame for flight in daylight conditions is reasonable. Operating the UAS in a 

tightly controlled area does not raise the type of risks that this section was intended to address, 

particularly given the size and speed of the UAS. Petitioner believes that an equivalent level of 

safety can be achieved by limiting flights to 50 minutes or 20% of batteiy power, whichever 

happens first. Petitioner notes that the Administrator has granted relief from this section on 

previous exemptions. 

6. 14 C.F.R. 91.405(a) Maintenance required; 14 C.F.R. § 91.407(a)(1) Opera.tion 

after maintenance, preventive maintenance, rebuilding or alteration; 14 C.F.R. 

&~ 91.409(a)(1) and (2) Inspections• 14 C.F.R. 91.417(a) and (b) Maintenance 

rP~nrcic. 

Maintenance will be accomplished by the operator pursuant to the applicable Operational 

Documents. An equivalent level of safety will be achieved because the UAS are very limited in 

size and will carry a small payload and operate only in restricted areas for limited periods of 

time. If inechanical issues arise, the UAS will be operating from no higher than 400 feet AGL 

and can immediately land. As provided in the applicable Operational Documents, the operator 

will ensure that the UAS is in working order prior to initiating flight, perform required 

maintenance, and keep a log of any maintenance performed. Moreover, the operator is the 

person most familiar with the aireraft and best suited to maintain the aircraft in an airworthy 

condition to provide the equivalent level of safety. As a result, an equivalent level of safety will 

be met by granting this exemption. Petitioner notes that the Administrator has granted relief 

froin this section in previous exemptions. 

7. Additional Relief. 

In addition to the exemptions listed above, the Petitioner requests exemption from such 

other rules and regulations as the FAA deems appropriate to enable the operations described 

herein. Since previous exemptions granted under Section 333 of the Reform Act have been 

effective for two years, the Petitioner also requests that if the FAA issues interim or final rules 

applicable to the operation of any UAS included herein after the Petitioner receives a Grant of 

Exemption that any conditions and limitations required in such Grant that are more burdensome 

than the new regulation be appropriately modified or removed. 

Expedited Process. 

Given that this exemption is similar to those that have already been granted and does not 

raise any novel issue, Petitioner requests that, if possible, this request for exemption be 

considered on an expedited basis. 

289143111 
U.S. Department of Transportation, Docket Operations 

September 11, 2015 

Page 7 

IX. Operating Parameters for UAS Use 

Petitioner proposes that if the requested exemptions are granted, it will operate the UAS 

under the following conditions: 

UAS operations will be conducted by a PIC. The PIC shall hold an airline transport, 

commercial, private, recreational, or sport pilot certificate. The PIC will also hold a 

current FAA airman medical certificate or a valid U.S. driver's license issued by a 

state, the District of Colombia, Puerto Rico, a territory, a possession, or the Federal 

government. The UAS will be in visual line of site (VLOS) of the PIC at all times. 

2. All UAS operations will utilize a visual observer ("VO"). The VO will not perform 

any other duties beyond assisting the PIC with seeing and avoiding air traffic and 

other ground-based obstacles/obstructions. 

3. The PIC and VO will be able to communicate verbally at all times. 

4. Petitioner will rely on a qualified vendor(s) to provide a pilot qualification program, 

including a training program incorporating proper aircraft operations and safety 

standards. The PIC and the VO will have obtained the necessary 

qualifications/training. A record of completion of this qualification process will be 

documented and made available to the Administrator upon request. 

5. UAS will not be flown at ground speeds exceeding 50 mph. 

6. Flights will be operated at an altitude of no more than 400 feet above ground level. 

7. Each UAS operation will be completed within 50 minutes flight time or with 20% 

battery power remaining, whichever occurs first. 

UAS will not be operated over any person (other than participating personnel) at an 

altitude that is hazardous to persons or property on the surface in the event of a UAS 

failure or emergency. UAS will be operated at a distance from participating buildings 

of at least 10 feet. Operations will be conducted at least 500 feet from nonparticipating persons or buildings, unless barriers are in place to provide adequate 

protection. 

9. The UAS will abort the flight in the event of unpredicted obstacles or emergencies in. 

accordance with the applicable Operational Document. 

280143111 
U.S. Department of Transportation, Docket Operations 

September 11, 2015 

Page 8 

10. The UAS will remain clear and yield the right of way to all other manned operations 

and activities at all times. 

11. UAS operations will not be conducted during night. 

12. The UAS will not be operated by the PIC from any moving device or vehicle. 

13. The UAS will not be operated less than 500 feet below or less than 2,000 feet 

horizontally from a cloud or when visibility is less than 3 statute miles from the PIC. 

14. The applicable Operational Documents and all documents required under 14 C.F.R. 

§ 91.9 and 91.203 will be available to the PIC at the Ground Control Station of the 

UAS any time the aircraft is operating. These documents will be made available to 

the Administrator upon request. 

15. Any incident, accident, or flight operation that transgresses the lateral or vertical 

boundaries of the operational area as defined by the applicable COA will be reported 

to the FAA's UAS Integration Office (AFS-80) within 24 hours. Accidents will be 

reported to the National Transportation Safety Board (NTSB). 

16. The operator will follow the procedures as outlined in its applicable Operational 

Documents. 

17. Prior to each flight, pilot will inspect the UAS to ensure it is in condition for safe 

flight. If the inspection reveals a discrepancy, the aircraft will be prohibited from 

operating until the necessary maintenance has been performed and the UAS is found 

to be in a condition for safe flight. 

18. All operations will be conducted over private or controlled-access property with 

permission from the land-owner/controller or authorized representative. Permission 

from the land-owner/controller or authorized representative will be obtained for each 

flight to be conducted. 

19. All maintenance and alterations will be properly documented in the aircraft records. 

20. Any UAS that undergoes maintenance or alterations that affect the UAS operation or 

flight characteristics will undergo a functional flight test in accordance with the 

applicable Operational Documents. 

28914311_1 
WI LLIAM S M U LLE N 

U.S. Department of Transportation, Docket Operations 

September 11, 2015 

Page 9 

21. Petitioner will institute a rigorous maintenance program to ensure airworthiness of the 

UAS. Operator will follow the manufacturer's UAS aircraft/component, 

maintenance, overhaul, replacement, inspection, and life limit requirements. 

22. Each UAS will comply with all manufacturer Safety Bulletins. 

X. Summary to be Published in Federal Register 

Petitioner: Pictometry International, Corp. 

Sections of 14 C. F. R. Affected: § 61.23 (a); § 61.23 (c); § 61.101(e)(4); § 61.1 O 1(e)(5); 

§ 61.113(a); 61.315(a); § 91.7(a); § 91.119(c); § 91.121; § 91.151(a)(1); § 91.405(a); 

§ 91.407(a)(1); § § 91.409(a)(1) and (2); § § 91.417(a) and (b). 

Description of Relief Sought: Petitioner seeks relief from the requirements of 14 C.F.R. 

§ 61.23(a); 14 C.F.R. § 61.23(c); 14 C.F.R. § 61.101(e)(4); 14 C.F.R. § 61.101(e)(5); 14 C.F.R. 

§ 61.113(a); 14 C.F.R. § 61.315(a); § 91.7(a);14 C.F.R. § 91.119(c); 14 C.F.R. § 91.121; 14 

C.F.R. § 91.151(a)(1); 14 C.F.R. § 91.405(a); 14 C.F.R. § 91.407(a)(1); 14 C.F.R. 

§§ 91.409(a)(1) and (2); 14 C.F.R. §§ 91.417(a) and (b) to use the UAS to conduct commercial 

aerial data collection as further described in Section III, subject to operating procedures that meet 

or exceed those that FAA requires for similar operations. 

XI. Conclusion 

Satisfaction of the criteria provided in Section 333 of the Reform Act regarding size, 

weight, speed, operating capabilities, proximity to airports and populated areas, operation within 

visual line of sight, and national security, provide more than adequate justification for the grant 

of the requested exemption allowing operation of Petitioner's UAS for the purposes set forth 

herein. Please contact Petitioner's outside counsel, Kevin D. Pomfret at 703-760-5204 or 

k]2omfret@williamsmullen.com with any questions about this filing. 

Sincere y, 

~ / in D. Pom ret 

KDP/kmb 

Attachment 

28914311_1 
U.S. Department of Transportation, Docket Operations 

September 11, 2015 

Page 10 

Attachment 1 

2_89143111 
Attachment l 

] , 2AgEagle 

2, 3D Robotics Aero-M 

3. 3D Robotics Iris 

4, 3D Robotics Iris+ 

5. 3D Robotics X8 

6. 3DRobot.ics Fixed Wing 

7, 3DRobotics Multirotor 

8. 3DRobotics Quadrotor 

9, 3DR Solo 

10. 3DR Spektre 

11, 3DRobotics Spektre Industrial Multi-Rotor Aer•ial Vehicic 

12. 3D Robotics Solo 

13. 3DRobotics X8+ 

14, 3D Robotics X8-M 

15, 3D Robotics Y6 

16. Aerial Mob Heavy Lifter 

17, Aerial Mob Liglht Lifter 

18. Aerial Remote Mineral Deteetion System (ARMDS) 

19. Aerialtronics Zenith with intergrated Airware system 

20, Aerialtronics Altura Zenith ATX8 

21, Aerigon 

22. Aerobo 

23, AeroCine Kopterworx Hammer X12 

24. Aeromao AeroMapper 300 

25, Aeromao Talon 

26, Aeromao Aerornapper 300 

27. Aeromao Aeroinapper BV-2 

28. AeroVironment Shrike 

29, AeroVironment Puma 

30, Aeronavics X4 Titanium 

31, Aeryon Sky Ranger 

32. Aervonics Sky Jib frame with a D.II A2 flight systern 

33. Aero-M 

34. Aeryon Scout 

35. Aeryon SkyRanger 

36, Ag.Eagle 

37. AgEagle Robotic 

38, AgScout 

39, AgScout Mini 

40, Agribotix Hornet Drone 

41. Agribotix Enduro Quad 

42. AgriView VK Ranger EX 
43, Aibot 

44, Aibotix X-6 

45. Air Rover AR-3000 

46, AirCover QR-425s 

47, AirRobot AR 180 

48, AirRobot AR 100 

49. AirRobot AR200 

50, Air-X 

51. Align M690 

52, Altavian Nova. 

53, Altavian Nova F6500 

54. Altavian Nova R8400 

55. Altus X-4 

56. Altus X-8 

57. American Drones, LLC Eagle 

58. Apprentice 

59, Arc11 Aerial OCTO multi-rotor UAS 

60. A7•ris lhexacoper 

61. AR-960 Hex Rotor 

62. AR-540 Quad Rotor 

63. ARF-MikroKopter OktoXL 

64, ARF-MikroKopter OktoXL + 

65. ArrowLite 

66, Asc'hec Falcon 

67. AscTec Falcon 8 

68, Astraeus Aerial Cinema System V.3CS 

69. Atlantic RC Aircraft LC04 

70, Auburn Trimble UX5 

71. Auburn War .Eagle 

72. Auburn EasyStar 

73. Auburn 

74, AV44 

75, Bixler 3DR Plane 

76. Blade 350QX 

77, Bixler 2 

78. Boomerang Carbon Fiber Frame (The ldentified System) 

79. Bormatec Maja UAV 

80. BOSH Technologies Super Swiper 

81. Bumblebee-S 

82. C-Astral Bramor gE0 

83. CarbonCore Octocopter 1000 

84. Carbon Core Cortex Quadcopter 

85. CCO w/Wkm M 

86. Chameleon Pro 
87. CinesStar 

88, Cinestar 6 

89, Cinestar X8 

90, Cinestar 8 

91, Cinestar 8 HL 

92. Cinestar 8 Okto XL 

93, Coaxial Quad Multirotor VAO1-V1 

94, Coaxial Quad Multirotor VA02-V2 

95, CopelandRED LLC Delta Wing Aircraft 

96. CyberQuad Maxi 

97. DJI Flame Wlieel F450 

98, DJ1 Flarne Wheel F550 

99, DAx8 

100, DJI inspire 

101. DJI Inspire 1 

102. DJI Irlspire 2 

103. DJI M P330z 

104. DJI Plhantom 

105. DJI Phantom 1 

106. DJI Phantom 2 

107, DJI Phantom 2+ 

108. DJI Phantom 2 Vision 

109, DJI Phantotn 2 Vision+ 

110. DJI Phantorn Vision + 

111. D,II Phantom 3 

112. DJI Phantom FC40 

113. DJI Spreading Wings S900 

114. DJI Spreading Wings S 1000 

115. DJI Spreading Wings S1000+ 

116, DJI S800 

117, DJI S800 EVO 

118. DJI T600 

119, Draganflyer Guardian 

120, Draganflyer X4ES 

121, Draganflyer X4P 

122, Draganflyer• X6 

123, DT-18 

124, DYS D800-X8 

125, Eagle VTOL 

126. Eagle V2 

127, E-.Flite Apprentice 

128, Event 38 E384 

129, F-450 

130. Falcon VTOL 
131, Fire Fly 6 

132, First Aerial Responder UAV 

133. Flarne Wheel G4 7,8 Skycrane 

134. Flying-Cam 3.0 SARAH 

135, Foxtech Kraken 130 V2 

136. FreeFly Systems ALTA RTF 

137. .FreeFly Systems Octocopter Airframe (Legacy) 

138, G4 

139. G4 models 

140. GeoStar 

141, GerMAP G220 

142. GerMAP G 180 

143, goFarm GF-1 

144. Gryphon Dynamics X8 

145. GT80X 

146, Harr•is 18 HL 

147, HEFF 

148, Helicopters West DJT Tnspire 

149. Helicopters West SkyJib 8 

150. Helios 960 

151. I-Iawkeye Mk-III 

152, T-TexaCrafter IIC-1 100 85. 

153, HexaCrafter HO-1250 

154, HH Blade 350QX2 AP 

155. Hobbyking "Bixler" Fixed Wing Trainer 

156, IloneyComb AgDrone 

157, I-Iorizon Hobby Blade 350 Qx2 quadcopter 

158, Hoverfly LiveSky, BigSky 60 and H-Frame 

159. Hubsan X4 micro drone 

160. I-IVP 14301 Multi Rotor 

161, Identified System 

162, IMT Global xFold Cinema 

163, Indago 

164. InovalDrone:Inova One 

165, I.nstantEye Mk-2 

166. InstantEye Mk-2 Gen2 

1.67. Intuitive Aerial Aeragon 

168. K 13 0 Octocopter 

169. KongCopter X8 

170. Kopterworx Hammer X 12 

171, Latitude I-1Q-4 I-lybrid Multirotor 

172. LB700 

173, Leading Edge Precision Vision 10 

174. Leptron Avenger 
175. Lewis Realty Associates Hexacopter 650 

176. Liberty l 

177. Lockheed Martin Desert Hawk III 

178, Lockheed Martin Indago 

179, Matrix quad copter 

180, MaxFlight 

181. MD4-200 

182. MD4-1000 

183. Mikrokopter 2.5 

184. MLB Company Super Bat 

185, MU-1H 

186. Multirotor G4 7.8 Skycrane 

187. Nighthawk 

188, Nighthawk VTOL 

189, OktoXL 6S 12 

190. PAG X4 

191, Parksone Radian R.TF 

192. Parrot Bebop drone 

193. Parrot PF 725100 Bebop Drone 14MP 

194, Parrot Skycontroller - 

195. Patriot X4 

196. Patriot X8 

197, Finwing Penguin V2 

198, Birdseyeview FireFly 6 

199, Phoenix 

200, Phoenix VTOL 

201. Phoenix 60 

202, Phoenix 60LE 

203. Pixllawk 

204, Precision Drone Pacesetter 

205, PrecisionHawk 

206, PrecisionHawk Hawkeye Mk-1I1 

207, PrecisionHawk Lancaster 

208. Precision Lancaster MK3 

209. Prioria Hex 

210. Prioria's Maveric 

211. Pulse Aerospace, PA 01 Vapor 

212. Pulse Aerospace Pulse Vapor 35 

213, Pulse Vapor 

214, Puma AE DDL 

215. PV 14817 Multi Rotor 

216. PV HLI 

217, PV HI.,2 

218. Q1 
21.9, Qua.deopter LLC MikroKopter 

220. Quiet UAV 

221, Qube 

222, R/C Rotors and Aerial Media; Matrix Prof, Multi Rotor Frame & Octo Heavy Lift Pro.f. 

Multi Rotor 

223. Frame Ronin Edition Microdrones:MD4-1000 

224, RC'I'imer I-Iexacopter 

225. RDASS 

226, REIIawk 500 

227, REIIawk 680 

228. RF-70 

229, Riegl RiCopter 

230. RITEWING Z3 Spade 47" 

231, Ritewing Drake 60" 

232, RITEWING Z3 Spade 70" 

233, RITEWING Z4 Spade 52" 

234, RMAX 

235. R.oboflight 

236. Rotomotion SR-15 

237. RV .Iet 

238. Scout X4 

239, SD02 

240, Seahawk 1.2 

241, SelectTech Geospacial's EH-4 

242, SenseFly eBee 

243. SenseFly eBee RTK 

244, SenseFly eXom 

245, Sensurion Magpie MP-1 

246. Service-Drone Recon One 

247. SeY•vice-Drone Blackbird 

248. SH 900 

249, ShadowHawlc 

250, Shrike 

251. Sirius 

252. SkyCatch 

253, SkyJib 8 v.2 Heavy Lifter 

254, SkyPhilly MI 

255, Skywalker Aero 

256. Slcywalker Flying Wing X8 

257. SnapRoll .Media SUAS 

258, Solutions Phoenix 30 

259. SteadiDrone 

260, Steadidrone Quad 

261. Steadydrone QU4D 
262. Steadidrone Mavik 

263, SuperX/P2 Multirotor 

264. Swift Radioplanes Lynx 

265, Tali 500 

266, Talon 120LE 

267. Tarot FY690S I-Iexacopter 

268, Tarot quadcopter 

269. Tarot 680pro 

270, Tarot 690 

271. Tarot 900 

272, Tarot 960 

273. Tarot T-15 

274. Tarot T15 C/F Folding Octocopter 

275, Tarot T18 UAV 

276, Tarot T690 

277. Tarot T810 

278. Tarot T960 

279. Tarsier Systems MoAC 

280. Tayzu Robotics Titan X8 

281. TBS Discovery Pro 

282. Team Black Sheep Discovery Pro Tarot T15 

283. T-Rex 700E F3C 

284, TREX 800E DFC PRO 

285. Trirnble UX5 

286. Trimble UX5 lip 

287. Trimble ZX5 

288. Turningy Talon 500 

289. TUP X8-800 

290, Turbo Ace CIN.EWING 6 

291, TurboAce Malrix-G quadcopter 

292. Turbo Ace inatrix-E 

293. Turbo Ace MATRIX-1 

294, UAV Solutions Phoenix 60 

295, Universeye Penguin 

296, Unmanned Flying Roiling Orb "UFRO" 

297, US2 GreenHawk 

298. UliliCopter ITX8 

299, VA03-vl 

300. VA04-v1 

301. VA07-vl 

302. Viking UAS Multicopter (VTOL) 

303. Vikin.g UAS FF-X4/X8 

304, VK-Patriot X4/X8 

305. Vilcing UAS Patriot X4/X8 M.ultirotor 
306. Viking UAS X6 Model 800 

307. Viking UAS Vilcing ONi; 

308, VK-450 

309, Viking Unmanned Aerial Systems, LLC AgriView VK Ranger EX 

310, Viking VK-FF-X4 

311, VK- Ranger EX- SAR Fixed Wing UAS 

312. Volantex Raptor Tarot T-18 

313, Volt Aerial R.obotics Octane 

314, Vulcan frame controlled by a DJI A2 flight controller 

31.5. Vulcan Mantis 

316, Vulcan Octocopter 

317. Vulcan Raven 

318, Vulcan UAV 

319, Walkera TALI HSO0 

320, Walkera Scout X4 

321. Wookong DJI 5800 

322, xCel Droncs XD550CDR 

323, XFold R.ig with four conFigui•ations: Quadcopter, Hexeopter, Oetocopter and x12 

Copter 

324. X8-M